AEROSPACE 508
Fall 2010
FOUNDATIONS
OF
FLUID MECHANICS
CENGIZ CAMCI
PROFESSOR OF AEROSPACE ENGINEERING
PLACE :
365 Willard
TIME :
9:45 – 11:00 am Tuesday &
Thursday
Cengiz Camci
Dept. of Aerospace Engineering
223 Hammond Building
University Park, PA, 16802
phone : 865 9871
cxc11@psu.edu
Office Hours :
11:00 – 12:00 pm
Tuesday & Thursday
and
by appointment
COURSE OUTLINE
BASIC CONSERVATION LAWS
INVISCID FLOWS
VISCOUS FLOWS
COMPRESSIBLE FLOWS
[ 9 LECTURES]
[ 6 LECTURES]
[ 9 LECTURES]
[ 7 LECTURES]
My own research interests
AEROTHERMODYNAMICS OF
TURBOMACHINERY AND HEAT TRANSFER
Cengiz Camci
Ph.D., Von Karman Institute for Fluid Dynamics, Brussels
Belgium
Research interests focus on studies in
fluid mechanics and heat transfer in
Aerospace Engineering
Turbomachinery/Rotorcraft/UAV systems.
RESEARCH ACTIVITIES
AEROSPACE ENGINEERING DEPARTMENT
AERONAUTICS
FL IGHT
VEHICLE DESIGN
ASTRONAUTICS
AIR
BREATHING
PROPUL SION
&
TURBOMACHINERY
ROTORCRAFT
ENGINEERING
EXPERIMENTAL
COMPUTATIONAL
ANAL YTICAL
FL UID MECHANICS
STRUCTURAL
DYNAMICS
AEROACOUSTICS
SPACECRAFT
&
SATELLITE DESIGN
ASTRODYNAMICS
DYNAMICS
&
CONTROLS
STRUCTURES
&
MATERIALS
HIGH PERFORMANCE COMPUTING
SPACE
PROPUL SION
COMPUTATIONAL
FL UIDS
&
RAREFIED GAS
DYNAMICS
SPACE
ENVIRONMENT
&
RE-ENTRY
TURBOMACHINERY AERODYNAMICS
& HEAT TRANSFER
CENGIZ CAMCI
TURBINE AERODYNAMICS
&
HEAT TRANSFER
HELICOPTER ROTOR
TEST RIG DEVELOPMENT
&
ICING STUDIES
COMPUTATIONAL
AERODYNAMICS OF
ROTATING ASDE
ANTENNAS
C. Camci
Axi al Fl ow Tu rbi ne
Research Facility
AFTRF
C. Camci
E.C.Smith & L.Long
(RCOE)
C. Camci
D.K.McLaughlin
K.Brentner
(RCOE)
SMALL
TURBOMACHINERY
&
OTHER MINIATURE
PROPULSION SYSTEMS
C.Camci
RTS
LARGE SCALE
COMPUTATION OF
ROTATING MACHINERY
FLOWS
C.Camci
24 Pro cessor C omp uter C luster
Ro to r Test Facility
AERO-THERMALMECHANICAL
OPTIMIZATION OF
STEAM TURBINE
BLADED DISK
ASSEMBLIES
C.Camci
T.Miller (ARL)
HEAT TRANSFER
&
FLUID MECHANICS
IN INTERNAL FLOWS
C.Camci
Ho t Air Win d Tu nn el
HAF
Most current research
•
as of August 2010
•
•
•
P&W HP turbine aerodynamics
non axisymmetric endwall contouring SIEMENS ENERGY
Ducted Fan Tip and Casing Region Improvements (USARO/VLRCOE)
•
Sand Erosion of Helicopter Balde Tip Region
(SIKORSKY/USARO/VLRCOE)
•
Axial Flow Turbine Experiments (GE CRD/ GE PS)
•
•
•
•
Squealer Tip Aerodynamics in Turbines (GE PS)
Turbine Tip Injection (DOE/SCIES)
ASDE-X (FAA) Airport Antenna Fluid Dynamics
Helicopter Rotor Test Facility (ARO/NASA)
Established capabilities:
36 inch Axial Flow Turbine Research Facility
Turbine aerodynamics/heat transfer/tip mitigation/secondary flow reduction/leakage flows
Axial Flow Fan Research Facility
Heat Transfer Wind Tunnel with heated air capability
Low Speed Turbine Cascade
High Speed Cascade Facility
Icing Test Facility (19 x 19 x 19 Cubic feet) -15 F capability
Currently for helicopter blade testing/instrument icing
25 Processor Xeon Cluster for High Performance Computations
3D Viscous Flows/time dependent flows/rotational frame/heat transfer
Established capabilities:
•
Sub-miniature aerodynamic probe making capability
•
Surface heat Transfer and shear stress measurement capability
•
Thermographic liquid crystals for surface Imaging
•
Pressure sensitive paints
•
Infrared Imaging
•
Planar Particle Image Velocimetry
•
Stereoscopic Particle Image Velocimetry
•
Turbomachinery performance tests
New Areas
• Sand Erosion on helicopter rotor blade tips
• Ducted Fan performance improvements for UAV applications
• Mems based rocket and propulsion system development
• Small Engine research for UAV/MAV propulsion
• Aerodynamics of rotating radar antennas ASDE-X
• Viscous flow predictions in rotating machinery (absolute frame)
TEXT BOOK :
Course notes will be available
Recommended software :
Multimedia Fluid Mechanics
Cambridge University Press
ISBN 0-521-78748-3
OTHER USEFUL BOOKS :
1) Incompressible Flow, R.L.Panton, Wiley Interscience
2) Viscous Fluid Flow, F.M.White, McGraw Hill
3) Modern Compressible Flow with Historical Perspective,
J.Anderson, McGraw Hill
4) Fundamental Mechanics of Fluids, I.G.Curie, McGraw Hill
5) Analytical Fluid Dynamics, G.Emanuel, CRC Press
Grading criteria :
HOMEWORK & PROJECTS
30/100
MIDTERM EXAMS
(20+20)/100
FINAL EXAM
30/100
COURSE OUTLINE
BASIC CONSERVATION LAWS
[ 9 LECTURES]
INVISCID FLOWS
[ 6 LECTURES]
VISCOUS FLOWS
[ 9 LECTURES]
COMPRESSIBLE FLOWS
[ 7 LECTURES]